BACKGROUND OF THE INVENTION
[0001] Since their introduction in the 1950s, airborne weather radar systems have primarily
provided an indication of weather "reflectivity" in the field of view of the radar.
Reflectivity is a radar parameter and is roughly correlated to rainfall rate. These
first radars displayed reflectivity only in grayscale and were not necessarily well
calibrated. However, in those early days, the ability to see where there was and wasn't
rainfall was a great improvement to flying blind or making very conservative circumnavigations
to avoid weather.
[0002] As weather radar evolved, improvements in the accuracy of reflectivity measurements
were made, along with improved display capability, first with the introduction of
digital radar, which provided monochromatic but discrete levels of reflectivity indication.
This was followed by the introduction of color displays allowing increasing reflectivity
levels to be displayed as green, yellow, and red.
[0003] In the 1980s several radars were introduced that provided turbulence detection capability.
The 1990s saw the introduction of predictive windshear detection and alerting capability
in some air transport category radars.
[0004] In 2004, Honeywell International, Inc. introduced a line of radars with volumetric
buffer capability, which made notable improvements in the display and analysis of
reflectivity data.
[0005] While these have all been significant improvements, the weather reflectivity and
turbulence display functions have some limitations with respect to the desired goal
of presenting to the crew a direct indication of hazards. For example:
● Reflectivity is not directly associated with hazard. In stratiform precipitation,
red level indications can often occur, although there is not necessarily a weather-related
hazard.
● Turbulence detection is limited in range to 40 NM (although some improvements may
be on the way to extend this to as far as 60 NM).
[0006] Conversely, there are weather hazards that are not associated with reflectivity or
turbulence levels that airborne weather radar can detect, most notably clear turbulence
(often due to nonprecipitation air mass boundaries or mountain-induced activity) and
also including icing conditions.
[0007] In any case, given the current operational environment with emphasis on on-time performance
and fuel efficiency, there is demand to provide the flight crew with as much information
as possible regarding weather hazards to ensure correct decision making.
SUMMARY OF THE INVENTION
[0008] The present invention provides a weather radar system for predicting existence of
lightning and hail weather conditions without range limits. An exemplary system generates
radar signals and receives weather radar reflectivity values based on the radar signals.
A processor receives and stores the weather radar reflectivity values into a three-dimensional
buffer, receives an outside air temperature value, and determines freezing level based
on the received outside air temperature value. The processor generates one or more
lightning icons when a reflectivity value, stored at one or more cells of the three-dimensional
buffer above the determined freezing level, is greater than a first threshold amount.
A display device displays the one or more lightning icons when an altitude value that
corresponds to the one or more cells associated with the generated lightning icons
has been selected for display.
[0009] In addition, the processor adds 1.6 kilometers (km) to the determined freezing level
and generates one or more hail icons, when a reflectivity value stored at one or more
cells of the three-dimensional buffer at the determined freezing level plus 1.6 km
is greater than a second threshold amount. The display device displays the one or
more hail icons when an altitude value that corresponds to the one or more cells associated
with the generated lightning icons has been selected for display.
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] Preferred and alternative embodiments of the present invention are described in detail
below with reference to the following drawings:
[0011] FIGURE 1 is a schematic block diagram of a system formed in accordance with an embodiment
of the present invention;
[0012] FIGURE 2 is a flowchart of an exemplary process performed by the system shown in
FIGURE 1;
[0013] FIGURE 3 is conceptual perspective view of layers of graphical representations of
the reflectivity values stored in the three-dimensional buffer; and
[0014] FIGURE 4 is an exemplary screen shot of a weather display that shows hail and lightning
icons generated upon inference of their existence.
DETAILED DESCRIPTION OF THE INVENTION
[0015] FIGURE 1 illustrates an embodiment of a weather display system 30 for providing improved
weather radar display functionality. The exemplary weather display system 30 includes
a weather radar system 40 and a display/interface front-end 38, and receives information
from an aircraft system 46. The display/interface front-end 38 includes a processor
42, memory 43, a display device 44, a user interface 48, and a database 32. An example
of the radar system 40 includes a radar controller 50 (coupled to the user interface
48), a transmitter 52, a receiver 54, and an antenna 56. The radar controller 50 controls
the transmitter 52 and the receiver 54 for performing the sending and receiving of
signals through the antenna 56. The weather radar system 40 and the display/interface
front-end 38 are electronically coupled to the aircraft system 46.
[0016] Radar relies on a transmission of a pulse of electromagnetic energy, referred to
herein as a signal. The antenna 56 narrowly focuses the transmission of the signal
pulse in comparison with the whole breadth of a desired downrange image. Like the
light from a flashlight, this narrow signal illuminates any objects in its path and
illuminated objects reflect the electromagnetic energy back to the antenna.
[0017] Reflectivity data correspond to that portion of a radar's signal reflected back to
the radar by liquids (e.g., rain) and/or frozen droplets (e.g., hail, sleet, and/or
snow) residing in a weather object, such as a cloud or storm, or residing in areas
proximate to the cloud or storm generating the liquids and/or frozen droplets.
[0018] The radar controller 50 calculates the distance of the weather object relative to
the antenna, based upon the length of time the transmitted signal pulse takes in the
transition from the antenna to the object and back to the antenna 56. The relationship
between distance and time is linear as the velocity of the signal is constant, approximately
the speed of light in a vacuum.
[0019] The memory 43 of the system 30 includes a three-dimensional volumetric buffer for
storing the reflectivity data. The system 30 has the capabilities of inferring lightning
and/or hail occurrence, based on the reflectivity values stored in the volumetric
buffer.
[0020] FIGURE 2 is a flowchart of an exemplary process 80 performed by the system shown
in FIGURE 1. First at a block 84, the processor 42 receives radar reflectivity values
from the radar system 40 and stores them in the three-dimensional buffer. Next, at
a block 86, the processor 42 determines the freezing level, based on present aircraft
altitude and current outside air temperature received from the aircraft system 46.
The freezing level is calculated from the current aircraft altitude and outside air
temperature using a standard lapse rateother temperature calculation models may be
used.
[0021] In one embodiment, lightning and hail determinations are performed simultaneously,
at decision block 87. For the lightning determination, the process 80 determines at
a decision block 88 if reflectivity values stored above determined freezing level
in the three-dimensional buffer are greater than a predefined amount. This condition
may also include the additional limitation of requiring a threshold number of adjacent
cells to have reflectivity values above the predefined amount. If a stored reflectivity
value is not greater than the predefined amount, then the process 80 returns to the
block 84 or to block 88 to check other cells. If a reflectivity value of a cell or
reflectivity values of a threshold number of adjacent cells is greater than the threshold
amount, then at a block 90 a lightning icon is generated and displayed on the weather
display (or multifunction display (MFD)). The process 80 then returns to the block
84 to repeat.
[0022] For the hail determination, 1.6 km is added to the freezing level, at a block 100.
Next, the process 80 determines at a decision block 102 if there exists proximate
cells within the three-dimensional buffer greater than a threshold number that include
reflectivity values greater than a threshold amount. A single cell could satisfy this
condition. If there are cells satisfying this condition, then the processor 42 generates
a hail icon(s) and displays it on the weather display or MFD, block 104. After block
104 or if the condition of the decision block 102 is not met, the process 80 returns
to block 84 to repeat.
[0023] In one embodiment, the reflectivity threshold for determining the existence of lightning
is set at 35 dBZ (decibels of Z (radar echo intensity/reflectivity)) and the lightning
reference altitude is set relative to the freezing level.
[0024] In one embodiment, an additional limitation is included before a determination of
possible existence of lightning. After block 88 in FIGURE 2, the processor 42 calculates
Echo top temperature and if the echo top temperature is colder than a threshold temperature
then the lightning icon is outputted. The echo top temperature could be calculated
from the following equation:

[0025] Echo top altitude may be determined using the stored reflectivity values in the three-dimensional
buffer or by analyzing the radar scan data as it is received. An example threshold
temperature is -20 C, but other temperatures may be used.
[0026] FIGURE 3 is a conceptual perspective view of planar slices 120 of reflectivity values
(cells) stored in the three-dimensional buffer. A hail reference altitude plane 126
is equivalent to the freezing level plus a threshold amount (e.g., 1.6 km). Other
threshold amounts may be used. In this example, the hail reference altitude plane
126 is an interpolation of the data in the planes above and below plane 126. If at
the plane 126 the reflectivity values for a threshold number of adjacent cells are
above a predefined reflectivity value, then they are inferred as a hail hazard area.
In one embodiment, the predefined reflectivity value for causing an inference of hail
is 45 dBZ.
[0027] FIGURE 4 is a screen shot (god's eye view) of a weather display 150 generated by
the system 30 of FIGURE 1, after it has been determined that lightning and hail inferences
have been determined using the radar reflectivity values stored in the three-dimensional
buffer. A lightning icon 154 is displayed to show lightning inferences. A hail icon
156 is displayed to show hail inferences.
[0028] In one embodiment, the three-dimensional buffer is not used. The system would analyze
either the radar reflectivity data associated with the freezing level or at the hail
reference altitude as soon as the data is received. Little or no buffering is performed.
[0029] Other altitudes relative to the freezing level can be used.
The embodiments of the invention in which an exclusive property or privilege is claimed
are defined as follows:
1. A method performed on an aircraft, the method comprising:
automatically receiving weather radar reflectivity values;
automatically receiving an outside air temperature value;
automatically determining freezing level based on the received outside air temperature
value;
automatically generating one or more lightning or hail icons when a received reflectivity
value is greater than a respective lightning or hail threshold amount based on the
determined freezing level; and automatically displaying the one or more lightning
or hail icons on a weather display based on a display selection.
2. The method of Claim 1, wherein the lightning threshold amount is within a threshold
amount from 35 dBZ.
3. The method of Claim 1, further comprising automatically storing the weather radar
reflectivity values into a three-dimensional buffer, wherein automatically generating
one or more hail icons comprises:
automatically adding a threshold value to the determined freezing level;
automatically generating one or more hail icons when a reflectivity value stored at
one or more cells of the three-dimensional buffer above determined freezing level
plus the threshold value is greater than a hail threshold amount; and
automatically displaying the one or more hail icons on the weather display when an
altitude value that corresponds to the one or more cells associated with the generated
hail icons has been selected for display.
4. The method of Claim 3, wherein automatically generating one or more hail icons further
comprises automatically generating one or more hail icons only when a threshold number
of adjacent cells includes reflectivity values greater than the hail threshold amount,
wherein the hail threshold amount is within a threshold amount from 45 dBZ, wherein
the threshold value is within a threshold from 1.6 km.
5. The method of Claim 1, wherein automatically generating one or more lightning icons
comprises generating the one or more lightning icons when the received reflectivity
value is greater than a respective lightning threshold amount above the determined
freezing level and an echo top temperature is less than an echo top temperature threshold.
6. A weather radar system having radar components for generating radar signals and receiving
weather radar reflectivity values based on the generated radar signals, the system
comprising:
a processor (42) in signal communication with the memory and the radar components,
the processor configured to:
receive weather radar reflectivity values;
receive an outside air temperature value;
determine freezing level based on the received outside air temperature value; and
generate one or more lightning or hail icons when a received reflectivity value is
greater than a respective lightning or hail threshold amount based on the determined
freezing level; and
a display device (44) in signal communication with the processor, the display device
configured to display the one or more lightning or hail icons based on a display selection.
7. The system of Claim 6, wherein the lighting threshold amount is within a threshold
amount from 35 dBZ.
8. The system of Claim 6, further comprising a memory comprising a three-dimensional
buffer, wherein the processor is further configured to:
add a threshold value to the determined freezing level; and
generate one or more hail icons when a reflectivity value stored at one or more cells
of the three-dimensional buffer at the determined freezing level plus the threshold
value is greater than the hail threshold amount; and
wherein the display device displays the one or more hail icons when an altitude value
that corresponds to the one or more cells associated with the generated hail icons
has been selected for display.
9. The system of Claim 8, wherein the processor generates one or more hail icons only
when a threshold number of adjacent cells include reflectivity values greater than
the hail threshold amount.
10. The system of Claim 8, wherein the hail threshold amount is within a threshold amount
from 45 dBZ.